Uses of Class
org.orekit.propagation.semianalytical.dsst.utilities.FieldAuxiliaryElements
Packages that use FieldAuxiliaryElements
Package
Description
This package provides force models for Draper Semi-analytical Satellite Theory (DSST).
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Uses of FieldAuxiliaryElements in org.orekit.propagation.semianalytical.dsst.forces
Methods in org.orekit.propagation.semianalytical.dsst.forces that return FieldAuxiliaryElementsModifier and TypeMethodDescriptionFieldForceModelContext.getFieldAuxiliaryElements()Method to get the auxiliary elementsrelated to theForceModelContext.Methods in org.orekit.propagation.semianalytical.dsst.forces with parameters of type FieldAuxiliaryElementsModifier and TypeMethodDescriptionprotected abstract <T extends CalculusFieldElement<T>>
T[]AbstractGaussianContribution.getLLimits(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements) Compute the limits in L, the true longitude, for integration.protected <T extends CalculusFieldElement<T>>
T[]DSSTAtmosphericDrag.getLLimits(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements) Compute the limits in L, the true longitude, for integration.protected <T extends CalculusFieldElement<T>>
T[]DSSTSolarRadiationPressure.getLLimits(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements) Compute the limits in L, the true longitude, for integration.<T extends CalculusFieldElement<T>>
T[]AbstractGaussianContribution.getMeanElementRate(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.<T extends CalculusFieldElement<T>>
T[]DSSTForceModel.getMeanElementRate(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.<T extends CalculusFieldElement<T>>
T[]DSSTJ2SquaredClosedForm.getMeanElementRate(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.<T extends CalculusFieldElement<T>>
T[]DSSTNewtonianAttraction.getMeanElementRate(FieldSpacecraftState<T> state, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.<T extends CalculusFieldElement<T>>
T[]DSSTTesseral.getMeanElementRate(FieldSpacecraftState<T> spacecraftState, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.<T extends CalculusFieldElement<T>>
T[]DSSTThirdBody.getMeanElementRate(FieldSpacecraftState<T> currentState, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.<T extends CalculusFieldElement<T>>
T[]DSSTZonal.getMeanElementRate(FieldSpacecraftState<T> spacecraftState, FieldAuxiliaryElements<T> auxiliaryElements, T[] parameters) Computes the mean equinoctial elements rates dai / dt.<T extends CalculusFieldElement<T>>
List<FieldShortPeriodTerms<T>> AbstractGaussianContribution.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.<T extends CalculusFieldElement<T>>
List<FieldShortPeriodTerms<T>> DSSTForceModel.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.<T extends CalculusFieldElement<T>>
List<FieldShortPeriodTerms<T>> DSSTJ2SquaredClosedForm.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.<T extends CalculusFieldElement<T>>
List<FieldShortPeriodTerms<T>> DSSTNewtonianAttraction.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.<T extends CalculusFieldElement<T>>
List<FieldShortPeriodTerms<T>> DSSTTesseral.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.<T extends CalculusFieldElement<T>>
List<FieldShortPeriodTerms<T>> DSSTThirdBody.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.<T extends CalculusFieldElement<T>>
List<FieldShortPeriodTerms<T>> DSSTZonal.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization prior to propagation for the current force model.default <T extends CalculusFieldElement<T>>
List<FieldShortPeriodTerms<T>> J2SquaredModel.initializeShortPeriodTerms(FieldAuxiliaryElements<T> auxiliaryElements, PropagationType type, T[] parameters) Performs initialization of J2-squared short period terms prior to propagation.Constructors in org.orekit.propagation.semianalytical.dsst.forces with parameters of type FieldAuxiliaryElementsModifierConstructorDescriptionFieldDSSTJ2SquaredClosedFormContext(FieldAuxiliaryElements<T> auxiliaryElements, UnnormalizedSphericalHarmonicsProvider provider) Simple constructor.FieldDSSTThirdBodyDynamicContext(FieldAuxiliaryElements<T> aux, CelestialBody body, T[] parameters) Constructor.protectedFieldForceModelContext(FieldAuxiliaryElements<T> auxiliaryElements) Simple constructor.